Aluminium alloy 2011 2011

Al-Cu-Bi-Pb alloy, AA 2011 / AlCu6BiPb family: Cu 5.0 to 6.0, Pb 0.2 to 0.6, Bi 0.2 to 0.6, Fe max 0.7, Si max 0.4, Zn 0 to 0.3 wt%, Al balance

Also known as UNS A92011, EN 3.1655, DIN AlCuBiPb, AFNOR A-U5PbBi, BS FC1, AA 2011 · 6 more

2011 (also written AlCu6BiPb, and sold as Avional in some catalogues) is a free-machining wrought aluminium alloy of the Al-Cu-Bi-Pb family, UNS A92011, WNR 3.1655.

8 sources · Updated 2026-10-26 · CC BY 4.0

Evidence level

2 of 5

Lab-measured

Machine it

Very good to excellent machinability

Carry load in the T6 temper

290 MPa yield

Weight

2.83 g/cm3

Heat

138 to 150 W/m.K

Soft form

350 MPa tensile in T4

Recipe, share of the weight

  • Al not statedAluminium
  • Cu not statedCopper
  • Pb not statedLead
  • Bi not statedBismuth
  • Fe not statedIron
  • Si not statedSilicon

Best for

Small, complex, high-precision machined parts made on automatic lathes, such as screws, bolts, gears, fasteners and fittings (suppliers rate machinability very good to excellent)

Weakest at

Weldability (rated poor to extremely poor by the sources) and corrosion resistance (rated low to moderate, and anodising or another surface treatment is advised)

Risk at a glance

  • People Low. Dust and fume warnings
  • If it fails Moderate. Poor weld joints
  • Corrosion Moderate. The Referans Metal T6 page rates corrosion resistance as Moderate.

Quick facts: 2011

Key properties of 2011
PropertyValueBasis
Density2.82 to 2.83 g/cm³3 sourced values across conditions
Yield strength140 to 300 MPa5 sourced values across conditions
Tensile strength245 to 420 MPa6 sourced values across conditions
Young's modulus70 to 71 GPa2 sourced values across conditions
Hardness (Brinell)97 to 110 HB3 sourced values across conditions
Thermal conductivity138 to 150 W/(m·K)3 sourced values across conditions
Thermal expansion (CTE)21.4 to 22.9 ppm/K2 sourced values across conditions
Melting point535 to 540 °C2 sourced values across conditions

What is the density of Aluminium alloy 2011?

Aluminium alloy 2011 has a density of 2.82 to 2.83 g/cm³. The range covers 3 sourced values across the tempers, forms and test conditions the sources report; room-temperature values are used where a source states a temperature.

What is the thermal conductivity of Aluminium alloy 2011?

Aluminium alloy 2011 has a thermal conductivity of 138 to 150 W/(m·K). The range covers 3 sourced values across the tempers, forms and test conditions the sources report; room-temperature values are used where a source states a temperature.

What is the coefficient of thermal expansion of Aluminium alloy 2011?

Aluminium alloy 2011 has a coefficient of thermal expansion of 21.4 to 22.9 ppm/K. The range covers 2 sourced values across the tempers, forms and test conditions the sources report; room-temperature values are used where a source states a temperature.

What is the melting point of Aluminium alloy 2011?

Aluminium alloy 2011 has a melting point of 535 to 540 °C. The range covers 2 sourced values across the tempers, forms and test conditions the sources report; room-temperature values are used where a source states a temperature.

What is the yield strength of Aluminium alloy 2011?

Aluminium alloy 2011 has a yield strength of 140 to 300 MPa. The range covers 5 sourced values across the tempers, forms and test conditions the sources report; room-temperature values are used where a source states a temperature.

What are the other names and codes for Aluminium alloy 2011?

Aluminium alloy 2011 is also written as UNS A92011, EN 3.1655, DIN AlCuBiPb, AFNOR A-U5PbBi, BS FC1, AA 2011. Each code is printed in the source listed beside it in the designations table.

What is Aluminium alloy 2011 used for?

Uses recorded in the sources include Brake pistons and clutch parts in brake systems; Pneumatic suspension parts; Fasteners and fittings, machined screws and bolts.

Why it exists

2011 is an old free-machining aluminium alloy. It is chosen for small, complex parts made on automatic lathes, where the free-machining additives give fast, clean cutting. Its copper content gives moderate strength, with a yield strength of 290 MPa and a tensile strength of 395 MPa in the T6 temper on one supplier page. The trade-off is weldability and corrosion resistance, which the sources rate low to poor, so the alloy is usually machined and then anodised or coated.

Where it's used

Automotive brake and suspension parts

The Applus datasheet names brake pistons, clutch parts in brake systems and parts for pneumatic suspensions among the applications of 2011.

Fasteners, fittings and precision machined parts

The Smith Metal datasheet lists fasteners and fittings, machine parts, automotive components and weaponry. Weerg suggests the alloy for gears, screws and bolts in automotive, aerospace and electronics work.

Recipe

Al-Cu-Bi-Pb alloy, AA 2011 / AlCu6BiPb family: Cu 5.0 to 6.0, Pb 0.2 to 0.6, Bi 0.2 to 0.6, Fe max 0.7, Si max 0.4, Zn 0 to 0.3 wt%, Al balance

2011 is a free-machining Al-Cu-Bi-Pb alloy. Copper gives strength, and lead and bismuth are added to make the chips break short for automatic lathes (Smith Metal and Referans Metal). The Applus datasheet also describes a solution anneal, water quench and hot ageing sequence, with temperatures printed in its heat treatment remark (not entered as properties). The composition below is the standard range, not a measured value.

What 2011 is made of
IngredientShare of the weightWhat it does
Aluminium Al not stated The matrix of the alloy. Balance of the composition.
Copper Cu not stated The main strengthening element, named first in the Referans Metal composition table and given the same range in the Smith Metal datasheet.
Lead Pb not stated Free-machining additive. It makes the chips break short, which is why the alloy machines so easily. The Hydro SDS lists lead as a carcinogen class for its family, but that entry describes a lower lead content.
Bismuth Bi not stated Free-machining additive that works with lead to improve chip breaking. Smith Metal and Total Materia both print the 0.2 to 0.6 % range.
Iron Fe not stated Impurity limit printed in the Referans Metal and Smith Metal composition tables.
Silicon Si not stated Impurity limit printed in the Referans Metal and Smith Metal composition tables.

Weight shares are as printed in the sources.

What it can do

Machine it

Very good to excellent machinability

Referans Metal rates machinability Very Good for T451 and T6, and Smith Metal calls it excellent and suitable for automatic lathes.

Carry load in the T6 temper

290 MPa yield

measured

The T6 page gives a yield strength of 290 MPa and a tensile strength of 395 MPa, with 17 % elongation over A50 mm.

Weight

2.83 g/cm3

measured

The T6 page and the Weerg datasheet both give a density of 2.83 g/cm3.

Heat

138 to 150 W/m.K

measured

Three sources give 138, 140 and 150 W/m.K (Smith Metal, Referans Metal T451 and T6), so the value depends on the source and temper.

Soft form

350 MPa tensile in T4

measured

Smith Metal gives a tensile strength of 350 MPa and a proof stress of 270 MPa for T4, with 18 % elongation at A5.

How it compares

2011 is the free-machining alloy in this collection. It gives up weldability and corrosion resistance for machinability, and suppliers rate it that way. Its sources do not compare it numerically with other grades.

The same measurements for each material, so you can compare them. Each row names the key condition under the value; the full conditions and methods are in the numbered notes under Technical details. Other materials are shown beside it; each was measured under its own conditions, so open its page before comparing closely. Compare every grade in the family.

Benchmarks
Measurement201160617075-T6202450525XXX2195 (Al-Cu-Li)Al1050201420172017A221923192618A300331034047501950565083AlMg2AlMg36013606360826101AA7050AA8011Au-Al IMCsAl master alloys
Thermal behavior and safety
Melting point, 2011 T451540 °C1no data532 °Cno data607.2 to 649 °Cno data1020 degF660 °C645 to 657 °C535 °C510 °C510 °C543 °C543 to 643 °C549 °C655 °C655 °C1068 to 1080 °F575 to 630 °C565 to 640 °C570 °C605 to 650 °C590 to 645 °C579 °C600 °C575 °C1090 °F490 °C640 to 655 °Cno data880 °C
Melting point, 2011535 °C2no data532 °Cno data607.2 to 649 °Cno data1020 degF660 °C645 to 657 °C535 °C510 °C510 °C543 °C543 to 643 °C549 °C655 °C655 °C1068 to 1080 °F575 to 630 °C565 to 640 °C570 °C605 to 650 °C590 to 645 °C579 °C600 °C575 °C1090 °F490 °C640 to 655 °Cno data880 °C
Thermal conductivity, 2011 T451Value printed on a supplier datasheet page140 W/m.K167 W/(m·K)130 W/m·K121 W/m-K138 W/m-K138 W/(m·K)no data220 W/(m·K)229 W/m.K138 W/(m·K)140 W/m.K140 W/m.K130 W.m/m2.°Cno data147 W/m.K190 W/m.K160 W/m.Kno data110 to 140 W/(m·K)109 to 117 W/(m·K)121 W/(m·K)138 W/(m·K)140 to 160 W/(m·K)164 W/(m·K)200 W/(m·K)180 W/(m·K)no data154 W/(m·K)210 to 220 W/(m·K)no datano data
Thermal conductivity, 2011 T6Value printed on a supplier datasheet page150 W/m.K167 W/(m·K)130 W/m·K121 W/m-K138 W/m-K138 W/(m·K)no data220 W/(m·K)229 W/m.K138 W/(m·K)140 W/m.K140 W/m.K130 W.m/m2.°Cno data147 W/m.K190 W/m.K160 W/m.Kno data110 to 140 W/(m·K)109 to 117 W/(m·K)121 W/(m·K)138 W/(m·K)140 to 160 W/(m·K)164 W/(m·K)200 W/(m·K)180 W/(m·K)no data154 W/(m·K)210 to 220 W/(m·K)no datano data
Thermal conductivity, 2011Value printed on a supplier datasheet page138 W/m.K167 W/(m·K)130 W/m·K121 W/m-K138 W/m-K138 W/(m·K)no data220 W/(m·K)229 W/m.K138 W/(m·K)140 W/m.K140 W/m.K130 W.m/m2.°Cno data147 W/m.K190 W/m.K160 W/m.Kno data110 to 140 W/(m·K)109 to 117 W/(m·K)121 W/(m·K)138 W/(m·K)140 to 160 W/(m·K)164 W/(m·K)200 W/(m·K)180 W/(m·K)no data154 W/(m·K)210 to 220 W/(m·K)no datano data
Physical and electrical
Density, 2011 T451Value printed on a supplier datasheet page2.82 g/cm³2.7 g/cm³2.8 Mg/m32.78 g/cc2.68 g/cc2.68 g/cm³0.096 lb/in32.7 g/cm³2.71 g/cm³2.82 g/cm³2.79 g/cm³2.79 g/cm³2.84 g/cm³2.84 g/cm³2.76 g/cm³2.73 g/cm³2.73 g/cm³2.65 g/cm³2.64 g/cm³2.64 g/cm³2.65 g/cm³2.69 g/cm³2.67 g/cm³2.71 g/cm³2700 kg/m32.7 g/cm³0.097 lb/cu.in2.83 g/cm³2.71 g/cm³no datano data
Density, 2011 T6Value printed on a supplier datasheet page2.83 g/cm³2.7 g/cm³2.8 Mg/m32.78 g/cc2.68 g/cc2.68 g/cm³0.096 lb/in32.7 g/cm³2.71 g/cm³2.82 g/cm³2.79 g/cm³2.79 g/cm³2.84 g/cm³2.84 g/cm³2.76 g/cm³2.73 g/cm³2.73 g/cm³2.65 g/cm³2.64 g/cm³2.64 g/cm³2.65 g/cm³2.69 g/cm³2.67 g/cm³2.71 g/cm³2700 kg/m32.7 g/cm³0.097 lb/cu.in2.83 g/cm³2.71 g/cm³no datano data
Density, 2011 (Weerg CNC datasheet)Value printed on a CNC supplier datasheet2.83 g/cm³2.7 g/cm³2.8 Mg/m32.78 g/cc2.68 g/cc2.68 g/cm³0.096 lb/in32.7 g/cm³2.71 g/cm³2.82 g/cm³2.79 g/cm³2.79 g/cm³2.84 g/cm³2.84 g/cm³2.76 g/cm³2.73 g/cm³2.73 g/cm³2.65 g/cm³2.64 g/cm³2.64 g/cm³2.65 g/cm³2.69 g/cm³2.67 g/cm³2.71 g/cm³2700 kg/m32.7 g/cm³0.097 lb/cu.in2.83 g/cm³2.71 g/cm³no datano data
Brinell hardness, 2011 T451Value printed on a supplier datasheet page105 HBno datano datano datano datano datano datano data35 HBno data105 HB105 HBno datano data120 HBno data45 HBno data65 to 95 HBno datano datano datano datano datano datano datano datano datano datano datano data
Brinell hardness, 2011 T6Value printed on a supplier datasheet page97 HBno datano datano datano datano datano datano data35 HBno data105 HB105 HBno datano data120 HBno data45 HBno data65 to 95 HBno datano datano datano datano datano datano datano datano datano datano datano data
Brinell hardness, 2011 T6 (Smith Metal)110 HB10no datano datano datano datano datano datano data35 HBno data105 HB105 HBno datano data120 HBno data45 HBno data65 to 95 HBno datano datano datano datano datano datano datano datano datano datano datano data
Other measurements
Coefficient of thermal expansion, 2011 T451Value printed on a supplier datasheet page21.4 µm/m.°C23.6 ppm/K23.4 µm/m·K23.2 ppm/K24.8 µm/m-°C24 ppm/Kno data22.5 ppm/K23.5 x10-6/K23 ppm/K22.9 µm/(m·°C)22.9 µm/m.°C22.5 x10^-6 m/m.°Cno data21.6 µm/m°C23.1 ppm/K23.1 x10-6/Kno datano data2.41×10^-5 1/K25 ppm/K23.8 µm/m/°C23.9 ppm/K21.7 µm/m°C23.5 ppm/K23.1 ppm/Kno data23.5 ppm/K2.35×10^-5 1/Kno datano data
Coefficient of thermal expansion, 2011 T6Value printed on a supplier datasheet page22.9 µm/m.°C23.6 ppm/K23.4 µm/m·K23.2 ppm/K24.8 µm/m-°C24 ppm/Kno data22.5 ppm/K23.5 x10-6/K23 ppm/K22.9 µm/(m·°C)22.9 µm/m.°C22.5 x10^-6 m/m.°Cno data21.6 µm/m°C23.1 ppm/K23.1 x10-6/Kno datano data2.41×10^-5 1/K25 ppm/K23.8 µm/m/°C23.9 ppm/K21.7 µm/m°C23.5 ppm/K23.1 ppm/Kno data23.5 ppm/K2.35×10^-5 1/Kno datano data
Modulus of elasticity, 2011 T451Value printed on a supplier datasheet page70 GPa68.9 GPa71 GPa73.1 GPa70.3 GPa70.3 GPa11 MSI69 GPa69000 MPa71 GPa72 GPa72 GPa73.8 x10^3 N/mm2no data71 GPa69.5 GPa69.5 GPano data70 GPa71 GPa72 GPa70 GPa70 GPa71 GPa69.5 GPa70 GPano data71.5 GPa70 GPano datano data
Modulus of elasticity, 2011Value printed on a supplier datasheet page71 GPa68.9 GPa71 GPa73.1 GPa70.3 GPa70.3 GPa11 MSI69 GPa69000 MPa71 GPa72 GPa72 GPa73.8 x10^3 N/mm2no data71 GPa69.5 GPa69.5 GPano data70 GPa71 GPa72 GPa70 GPa70 GPa71 GPa69.5 GPa70 GPano data71.5 GPa70 GPano datano data
Yield strength, 2011 T451140 MPa3276 MPa503 MPa324 MPa13 ksi193 MPa74 ksi29 MPa> 85 MPa> 400 MPa276 MPa276 MPa> 50 ksi70 MPa350 MPa50 MPa> 110 MPa55 MPano datano data> 125 MPa> 120 MPa> 80 MPa350 MPa21 ksi> 255 MPa28000 psi> 414 MPano datano datano data
Ultimate tensile strength, 2011 T451Value printed on a supplier datasheet page300 MPa310 MPa572 MPa469 MPa28 ksi228 MPa80 ksi88 MPa105 to 145 MPa> 460 MPa427 MPa427 MPa> 62 ksi160 MPa420 MPa110 MPa> 140 MPa124 MPa270 to 350 MPa300 MPa275 to 350 MPa190 to 230 MPa190 to 260 MPa410 MPa27 ksi> 300 MPa32000 psi> 483 MPa180 to 195 MPano datano data
Elongation, 2011 T451Value printed on a supplier datasheet page16 %17 %11 %19 %25 %12 %8 %50 to 65 %4 to 8 %> 6 %18 %18 %> 6 %12 %> 5 %25 %> 8 %12 %> 2 %20 %> 12 %4 to 12 %> 12 %4 %8 %> 9 %> 8 %> 7 %> 1 %no datano data
Yield strength, 2011 T6Value printed on a supplier datasheet page290 MPa4276 MPa503 MPa324 MPa13 ksi193 MPa74 ksi29 MPa> 85 MPa> 400 MPa276 MPa276 MPa> 50 ksi70 MPa350 MPa50 MPa> 110 MPa55 MPano datano data> 125 MPa> 120 MPa> 80 MPa350 MPa21 ksi> 255 MPa28000 psi> 414 MPano datano datano data
Ultimate tensile strength, 2011 T6Value printed on a supplier datasheet page395 MPa310 MPa572 MPa469 MPa28 ksi228 MPa80 ksi88 MPa105 to 145 MPa> 460 MPa427 MPa427 MPa> 62 ksi160 MPa420 MPa110 MPa> 140 MPa124 MPa270 to 350 MPa300 MPa275 to 350 MPa190 to 230 MPa190 to 260 MPa410 MPa27 ksi> 300 MPa32000 psi> 483 MPa180 to 195 MPano datano data
Elongation, 2011 T6Value printed on a supplier datasheet page17 %17 %11 %19 %25 %12 %8 %50 to 65 %4 to 8 %> 6 %18 %18 %> 6 %12 %> 5 %25 %> 8 %12 %> 2 %20 %> 12 %4 to 12 %> 12 %4 %8 %> 9 %> 8 %> 7 %> 1 %no datano data
Minimum yield strength, 2011 T6, thickness over 3.17 up to 38.1 mm> 260 MPa5276 MPa503 MPa324 MPa13 ksi193 MPa74 ksi29 MPa> 85 MPa> 400 MPa276 MPa276 MPa> 50 ksi70 MPa350 MPa50 MPa> 110 MPa55 MPano datano data> 125 MPa> 120 MPa> 80 MPa350 MPa21 ksi> 255 MPa28000 psi> 414 MPano datano datano data
Minimum tensile strength, 2011 T6, thickness over 3.17 up to 38.1 mm> 310 MPa6310 MPa572 MPa469 MPa28 ksi228 MPa80 ksi88 MPa105 to 145 MPa> 460 MPa427 MPa427 MPa> 62 ksi160 MPa420 MPa110 MPa> 140 MPa124 MPa270 to 350 MPa300 MPa275 to 350 MPa190 to 230 MPa190 to 260 MPa410 MPa27 ksi> 300 MPa32000 psi> 483 MPa180 to 195 MPano datano data
Tensile strength, 2011 T3365 MPa7310 MPa572 MPa469 MPa28 ksi228 MPa80 ksi88 MPa105 to 145 MPa> 460 MPa427 MPa427 MPa> 62 ksi160 MPa420 MPa110 MPa> 140 MPa124 MPa270 to 350 MPa300 MPa275 to 350 MPa190 to 230 MPa190 to 260 MPa410 MPa27 ksi> 300 MPa32000 psi> 483 MPa180 to 195 MPano datano data
Tensile strength, 2011 T8420 MPa8310 MPa572 MPa469 MPa28 ksi228 MPa80 ksi88 MPa105 to 145 MPa> 460 MPa427 MPa427 MPa> 62 ksi160 MPa420 MPa110 MPa> 140 MPa124 MPa270 to 350 MPa300 MPa275 to 350 MPa190 to 230 MPa190 to 260 MPa410 MPa27 ksi> 300 MPa32000 psi> 483 MPa180 to 195 MPano datano data
Proof stress, 2011 T6300 MPa9276 MPa503 MPa324 MPa13 ksi193 MPa74 ksi29 MPa> 85 MPa> 400 MPa276 MPa276 MPa> 50 ksi70 MPa350 MPa50 MPa> 110 MPa55 MPano datano data> 125 MPa> 120 MPa> 80 MPa350 MPa21 ksi> 255 MPa28000 psi> 414 MPano datano datano data
Tensile strength, 2011 (Weerg CNC datasheet)245 MPa11310 MPa572 MPa469 MPa28 ksi228 MPa80 ksi88 MPa105 to 145 MPa> 460 MPa427 MPa427 MPa> 62 ksi160 MPa420 MPa110 MPa> 140 MPa124 MPa270 to 350 MPa300 MPa275 to 350 MPa190 to 230 MPa190 to 260 MPa410 MPa27 ksi> 300 MPa32000 psi> 483 MPa180 to 195 MPano datano data
Yield strength, 2011 (Weerg CNC datasheet)200 MPa12276 MPa503 MPa324 MPa13 ksi193 MPa74 ksi29 MPa> 85 MPa> 400 MPa276 MPa276 MPa> 50 ksi70 MPa350 MPa50 MPa> 110 MPa55 MPano datano data> 125 MPa> 120 MPa> 80 MPa350 MPa21 ksi> 255 MPa28000 psi> 414 MPano datano datano data

Why choose it, and why not

Good for

  • Small machined parts on automatic lathes: suppliers rate machinability very good to excellent.
  • Brake and suspension parts, as named in the Applus datasheet.
  • Fasteners, fittings, screws and bolts, as named in the Smith Metal and Weerg datasheets.

Watch out for

  • Weldability: rated low to extremely poor, and welding is seldom suitable.
  • Corrosion: rated low to moderate, and the sources advise anodising or another surface treatment.
  • Temper dependence: the T451 page prints 140 MPa yield against 290 MPa for T6, so check the temper before comparing.
  • Spacecraft or launcher use of the 2011 grade is not confirmed by any source read here.

2011 is a free-machining copper alloy for small precision parts made on automatic lathes. It is poor to weld and only low to moderate in corrosion resistance, so it is machined and then protected, and the sources here do not confirm a flight record.

Technical details

For scientists and researchers. Everything above comes from the record below: every number with its method, its conditions and its source.

Other names and standards

The same grade under other systems, as datasheets and standards print them. Each code was checked against the page it comes from.

Other names and standards
SystemCodes
UNSA92011
EN3.1655
DINAlCuBiPb
AFNORA-U5PbBi
BSFC1
AA2011
ISOAlCu6BiPb
AMSQQ-A-225/3 (Cold-drawn round bar, sheet and wire, T6)
ASTMB221 (Extruded round bar, sheet, wire and tube), B211 (Cold-drawn round bar, sheet, wire), B210 (Cold-drawn tube)
Trade nameAvional

Notes

The method, full conditions and any caveat for the numbered rows above.

Notes for the numbered rows
#MeasurementMethodConditionsCaveat
1Melting point, 2011 T451Single value printed on a supplier datasheet pagetemper T451 (page title)form not stated—
2Melting point, 2011Single value printed on a supplier datasheet pagetemper not stated—
3Yield strength, 2011 T451Value printed on a supplier datasheet page; it conflicts with the T6 and Smith values, see gapstemper T451 (page title)form not statedmeasure not stated—
4Yield strength, 2011 T6—temper T6 (page title)form not statedmeasure not stated—
5Minimum yield strength, 2011 T6, thickness over 3.17 up to 38.1 mmMinimum value printed in the delivery table of a supplier datasheet pagetemper T6 (page title)thickness over 3.17 up to and including 38.1 mm (decimal commas in the source)basis minimum delivery value—
6Minimum tensile strength, 2011 T6, thickness over 3.17 up to 38.1 mmMinimum value printed in the delivery table of a supplier datasheet pagetemper T6 (page title)thickness over 3.17 up to and including 38.1 mm (decimal commas in the source)basis minimum delivery value—
7Tensile strength, 2011 T3Value printed in the Mechanical Properties table of the Smith Metal datasheettemper T3form not stated—
8Tensile strength, 2011 T8Value printed in the Mechanical Properties table of the Smith Metal datasheettemper T8form not stated—
9Proof stress, 2011 T6Proof stress printed in the Mechanical Properties table of the Smith Metal datasheettemper T6form not stated—
10Brinell hardness, 2011 T6 (Smith Metal)Value printed in the Mechanical Properties table of the Smith Metal datasheettemper T6form not stated—
11Tensile strength, 2011 (Weerg CNC datasheet)Value printed in the mechanical properties table of a CNC supplier datasheettemper not statedtest ISO 6892—
12Yield strength, 2011 (Weerg CNC datasheet)Value printed in the mechanical properties table of a CNC supplier datasheettemper not statedtest ISO 6892—

Corrosion and compatibility

What happens when it meets other materials and environments.

Corrosion and compatibility
EnvironmentConcernWhat happens
General service (supplier selection factor, no test conditions) for 2011 T451 low The Referans Metal T451 page rates corrosion resistance as Low.1
General service (supplier selection factor, no test conditions) for 2011 T6 moderate The Referans Metal T6 page rates corrosion resistance as Moderate.2
General service, bare or unanodised surface low Smith Metal rates the corrosion resistance of 2011 as poor and says anodising is needed for surface protection.3
Surface finishing and exposure where corrosive attack can be expected low The Applus datasheet says a surface treatment is always recommended, and that anodising for decorative purposes is not possible.4
Corrosion details
#EnvironmentDetailsTest conditions
1 General service (supplier selection factor, no test conditions) for 2011 T451 The key characteristics list for 2011 T451 prints Corrosion Resistance Low, alongside Machinability Very Good, Weldability Low, Formability Moderate and Strength Good. No test environment, exposure time or rate is given. basis qualitative selection factor onlytest none statedtemper T451
2 General service (supplier selection factor, no test conditions) for 2011 T6 The characteristic properties list for 2011 T6 prints Corrosion Resistance Moderate, Weldability Poor and Machinability Very Good. The T451 page prints Low for the same alloy, so the two temper pages disagree. basis qualitative selection factor onlytest none statedtemper T6
3 General service, bare or unanodised surface The Smith Metal datasheet lists Poor corrosion resistance and states that the alloy displays poor corrosion resistance, so anodising will be required for additional surface protection. No test environment or exposure time is given. basis qualitative supplier statementtest none stated
4 Surface finishing and exposure where corrosive attack can be expected The datasheet says a surface treatment is always recommended where corrosive attack can be expected, that corrosion resistance under certain conditions is insufficient, and that anodising for decorative purposes is not possible. No test data are given. basis qualitative datasheet statementtest none stated

Risks and side effects

Hazards to people, what happens when a cell overheats, and how the material is handled and stored.

For people

The Hydro safety data sheet for the 2xxx series gives dust, fume and environmental warnings for processing. No health data for the 2011 grade itself were found.

Machining dust
Metallic dust can ignite or explode, and dusts and fumes from machining or welding can cause metal fume fever (Hydro SDS, 2xxx series).
Lead content
The family sheet lists lead as Carc. 1B (H350) at below 0.05 %, but this grade contains 0.2 to 0.6 % lead, so that sheet does not describe it. Treat chips and dust as lead-bearing.
Environment
Small chips, fine turnings and processing dust may be toxic to aquatic life, according to the same sheet.

If it fails

The failure routes found in the sources are weld joints and surface corrosion.

Welds
Smith Metal rates weldability extremely poor, and the Referans Metal pages rate it Low and Poor. Welding is seldom needed because the alloy is used as machined parts.
Corrosion
The sources rate corrosion resistance low to moderate and advise a surface treatment. No salt-spray or exposure test for this alloy was found.

Handling and storage

Specify temper and form
The yield and tensile values depend on the temper and product form, so state T451, T6, T3, T8, bar or tube when comparing figures.
Dust control
Keep machining dust and fines under control, and do not breathe dust or fume, following the Hydro SDS.

Test details
The original wording and numbers from the sources, for readers who want them.

Failure risks

Failure risks
FailureTrigger and consequence
Poor weld jointsmoderate severityFusion welding of 2011 partsThe sources rate weldability Low (T451 page), Poor (T6 page) and Extremely poor (Smith Metal), and Smith Metal says welding is seldom necessary because the alloy is used mainly as machined parts. No weld-strength figure was found.
Surface corrosion of unprotected partsmoderate severityLong exposure in service environments without anodising or another coatingThe sources rate corrosion resistance low to moderate and say a surface treatment is needed. No rate, pit depth or test result for this alloy was found, so the risk is qualitative only.

Handling and storage

  • Keep machining dust, chips and fines under control. The Hydro sheet says that metallic dusts may ignite or explode, that product dust is combustible, and that chips and turnings may be toxic to aquatic life.
  • Specify the temper and product form before comparing values. The Referans Metal pages print a yield strength of 140 MPa for T451 and 290 MPa for T6, and the Smith Metal table gives proof stress of 270 to 315 MPa across T3 to T8.

Mitigations

  • Anodise or otherwise coat parts for surface protection. Smith Metal says anodising will be required, while Applus says decorative anodising is not possible for this alloy.

Supply and geography

How common the raw materials are and where they come from.

Primary aluminium smelter production, 2025 estimate (world)

Top producers (2025)
China 60.8%, India 5.7%, Russia 5.3%, Canada 4.5%, United Arab Emirates 3.6%
Recycling
USGS: in 2025 about 3.6 million tons of aluminum were recovered from purchased scrap in the United States, about 56 % from new scrap and 44 % from old scrap. Old-scrap recovery was equivalent to about 28 % of apparent consumption.
Substitutes
USGS: composites can substitute for aluminum in aircraft fuselages and wings. Copper can replace aluminum in electrical and heat-exchange applications.